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NOTE: See Figure 518.
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
NOTE: An example of how to use the Elevator Tab Rig Adjustment Chart is shown with the
dashed lines with arrows.
The example assumes 9.5 airplane nose down handwheel turns are needed to retrim the
airplane with a center of gravity of 20 percent MAC on the left chart. Follow the diagonal
lines to the left side of the right chart. Make a horizontal line across the chart. Draw a
line down from the point where the horizontal line intersects the thick diagonal line on
the right chart.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 598.30
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
(Continued)
The example shows that you will need to adjust the elevator tab to 0.11 inches (2.8 mm)
trailing edge up from the current position to bring the airplane to a neutral elevator tab
trim.
NOTE: For coarse adjustment, a half turn of the tab rod end results in approximately 0.10 inch
(2.5 mm) at the tab trailing edge .
For finer adjustment, one full turn of the bushing [104] (vernier collar) results in
approximately 0.02 inch (0.5 mm) at the elevator tab trailing edge Figure 508 or
Figure 509.
The number of threads showing on the pushrod ends should be approximately equal to
the number of threads showing on the bushing [104].
The elevator tab should be adjusted to the nearest 0.01 inch (0.3 mm) shown on the scale
at the bottom of the right chart of the Elevator Tab Rig Adjustment Chart.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080;
AIRPLANES WITH SIX HINGE ELEVATOR TABS
SUBTASK 27-31-00-820-028
(11) Adjust the elevator tab pushrods [110] using the Elevator Tab Rig Adjustment Chart.
GUN 101-122
NOTE: See Figure 517.
GUN 001-099, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 519.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080;
AIRPLANES WITH SIX HINGE ELEVATOR TABS
NOTE: An example of how to use the Elevator Tab Rig Adjustment Chart is shown with the
dashed lines with arrows.
The example assumes 10.5 airplane nose down handwheel turns are needed to retrim
the airplane with a center of gravity of 20 percent MAC on the left chart. Follow the
diagonal lines to the left side of the right chart. Make a horizontal line across the chart.
Draw a line down from the point where the horizontal line intersects the thick diagonal
line on the right chart.
The example shows that you will need to adjust the elevator tab to 0.11 inches (2.8 mm)
trailing edge up from the current position to bring the airplane to a neutral elevator tab
trim.
NOTE: For coarse adjustment, a half turn of the tab rod end results in approximately 0.10 inch
(2.5 mm) at the tab trailing edge Figure 511.
For finer adjustment, one full turn of the bushing [104] (vernier collar) results in
approximately 0.02 inch (0.5 mm) at the elevator tab trailing edge.
The number of threads showing on the pushrod ends should be approximately equal to
the number of threads showing on the bushing [104].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 598.31
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080; AIRPLANES
WITH SIX HINGE ELEVATOR TABS (Continued)
The elevator tab should be adjusted to the nearest 0.01 inch (0.3 mm) shown on the scale
at the bottom of the right chart of the Elevator Tab Rig Adjustment Chart.
GUN ALL
SUBTASK 27-31-00-820-014
(12) If it is necessary, do this coarse adjustment of the elevator tab pushrods:
GUN 156, 201-204, 206 PRE SB 737-55A1080
NOTE: See Figure 508 or Figure 509.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 511.
GUN 101-122
NOTE: See Figure 517.
GUN 156, 201-204, 206 PRE SB 737-55A1080
NOTE: See Figure 518.
GUN 001-099, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 519.
GUN ALL
(a) Remove the pins [111], nuts [109], washers [108], bolts [106], and bushings [107] from the
tab pushrods [110].
(b) Turn the tab pushrod ends until the adjustment dimension is within 0.1 inch (3 millimeters).
NOTE: One half turn of the tab pushrod end is equal to 0.1 inch (3 mm) at the elevator tab
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(15)
